FIELD: tactical missile weaponry. SUBSTANCE: the method consists in missile flight to the target with lateral attitude stabilization of the nose section provided with a homing head. The nose section is joined to the other missile sections through a cylindrical hinge joint, and lateral attitude stabilization of the nose section is accomplished by aerodynamic and/or gas dynamic control surfaces of this section. EFFECT: enhanced accuracy of hitting of small-sized and moving targets. 3 cl, 3 dwg
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